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This section includes InterviewSolutions, each offering curated multiple-choice questions to sharpen your knowledge and support exam preparation. Choose a topic below to get started.

51.

Expand divergence of velocity ∇.\(\vec{V}\) for a one-dimensional flow.(a) \(\frac{\partial u}{\partial x}+\frac{\partial v}{\partial y}+\frac{\partial w}{\partial z}\)(b) \(\frac{\partial u}{\partial x}\)(c) \(\frac{du}{dx}+\frac{dv}{dy}+\frac{dw}{dz}\)(d) \(\frac{D\vec{V}}{Dt}\)This question was posed to me at a job interview.My query is from Governing Equations topic in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct option is (b) \(\frac{\partial u}{\partial X}\)

Explanation: Here,

\(\frac{\partial}{\partial x}\VEC{i}+\frac{\partial}{\partial y}\vec{j}+\frac{\partial}{\partial z}\vec{K}\)

\(\vec{V}= u\vec{i} +v\vec{j}+W\vec{k}\)

∇.\(\vec{V}=\frac{\partial u}{\partial x}+\frac{\partial v}{\partial y}+\frac{\partial w}{\partial z}\)

For one-dimensional flow,

∇.\(\vec{V}=\frac{\partial u}{\partial x}\).

52.

In the general transport equation, ϕ is the flow property. To get the energy equation out of this general equation, which of these variables cannot be used?(a) v(b) T(c) h0(d) iI have been asked this question by my school principal while I was bunking the class.My question is taken from Energy Equation in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» CORRECT choice is (a) v

The EXPLANATION: T, h0 and I represent temperature, total ENTHALPY and internal energy. These can be used to get the energy equation. Y-velocity component (v) cannot be used. It will result in the y-momentum equation.
53.

The rate of heat increase in a system depends on __________(a) the rate of heat transferred to the system(b) the rate of heat generated by the system(c) neither the rate of heat generated by the system nor the rate of heat transferred to the system(d) both the rate of heat transferred to the system and the rate of heat generated by the systemThis question was posed to me in an interview for internship.I would like to ask this question from Energy Equation topic in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The CORRECT choice is (d) both the RATE of heat transferred to the system and the rate of heat generated by the system

To explain I WOULD SAY: Heat can be added to a system in two ways:

 Transfer of heat across the SURFACE of the element by surface forces.

 The heat generated by the system itself.

54.

The physical property Φof the general transport equation is replaced by ________ to get momentum equation.(a) Velocity vector(b) Mass(c) Force vector(d) Acceleration vectorThe question was asked in an international level competition.The doubt is from Momentum Equation in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The CORRECT OPTION is (a) Velocity vector

Best explanation: The physical property in general transport equation should be REPLACED by velocity vector. This will result in momentum equation. For mass CONSERVATION, Φ = 1. For momentum (mass×velocity) conservation, Φ = 1×\(\vec{V}=\vec{V}\).

55.

We can describe the state of a substance in thermodynamic equilibrium using two state variables. What are these two variables?(a) Density and temperature(b) Density and pressure(c) Pressure and Temperature(d) Velocity and TemperatureThis question was posed to me at a job interview.My question is based upon Equations of State topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct OPTION is (a) Density and temperature

Easy explanation: There are FOUR thermodynamic VARIABLES – density, temperature, pressure and specific internal energy. Among these, pressure and specific internal energy can be REPRESENTED USING density and temperature.

56.

Euler equations govern ____________ flows.(a) Viscous adiabatic flows(b) Inviscid flows(c) Adiabatic and inviscid flows(d) Adiabatic flowsI got this question in exam.My question comes from Euler Equation topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The CORRECT OPTION is (c) ADIABATIC and inviscid flows

For explanation I would say: Euler equations constitute the governing equations of flow for adiabatic and inviscid flows. Here, the dissipative transport of flow PROPERTIES is neglected.

57.

Which of the variables in the equation \(\rho\frac{Du}{Dt}=-\frac{\partial p}{\partial x}+\frac{\partial \tau_{xx}}{\partial x}+\frac{\partial \tau_{yx}}{\partial y}+\frac{\partial \tau_{zx}}{\partial z}+\rho f_x\) will become zero for formulating Euler equation?(a) fx, τyx, τzx(b) τxx, τyx, u(c) τxx, τyx, τzx(d) τxx, p, τzxI have been asked this question in semester exam.I'd like to ask this question from Euler Equation in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct option is (c) τxx, τyx, τzx

To explain I would SAY: τxx, τyx, τzx represent shear stresses DUE to VISCOUS effects; u is the x-velocity; fx is the body force and P is the PRESSURE. τxx,τyx,τzx should become zero for the flow to be in-viscid and the equations to be Eulerian.

58.

Euler form of momentum equations does not involve this property.(a) Stress(b) Friction(c) Strain(d) TemperatureThe question was asked in an interview.I want to ask this question from Euler Equation topic in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» CORRECT choice is (b) Friction

The explanation is: Euler form of equations is for inviscid FLOWS. For inviscid flows, VISCOSITY is ZERO. So, there are no friction terms INVOLVED.
59.

According to the conservation law, “Net mass flow across the fluid element is equal to the rate of change of mass inside the element”. But, stating the final equation, “Net mass flow across the fluid element + the rate of change of mass inside the element = 0”. Why is the operation not subtraction?(a) Irrespective of the law, the sum is always zero(b) The two terms are always opposite in sign(c) Change in sign is not considered(d) Rate of change may be increase or decreaseThe question was posed to me in unit test.The question is from Continuity Equation in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct option is (b) The two terms are ALWAYS opposite in sign

The explanation: The “net mass FLOW ACROSS the fluid element” being positive means that it is outward flow. If flow is outward, mass inside the fluid element decreases leading to a NEGATIVE “rate of change of mass inside the element”. Thus, the two terms are always opposite in sign that they can be SUMMED up to get zero.

60.

Consider an infinitesimally small fluid element with density ρ (of dimensions dx, dy and dz) fixed in space and fluid is moving across this element with a velocity \(\vec{V}=u\vec{i}+v\vec{j}+w\vec{k}\). The net mass flow across the fluid element is given by ______(a) \([\frac{\partial(\rho u)}{\partial x} + \frac{\partial(\rho v)}{\partial y} + \frac{\partial(\rho w)}{\partial z}]dx \,dy \,dz\)(b) \([\frac{\partial(\rho u)}{\partial x} + \frac{\partial(\rho v)}{\partial y} + \frac{\partial(\rho w)}{\partial z}]\)(c) [ρ]dx dy dz(d) \([\frac{\partial(\rho)}{\partial x} + \frac{\partial(\rho)}{\partial y} + \frac{\partial(\rho)}{\partial z}]dx \,dy \,dz\)This question was posed to me in semester exam.This is a very interesting question from Continuity Equation in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»
61.

The time rate of change of a control volume moving along with the flow is represented by substantial derivative. Why?(a) Because the change is substantial(b) Because the change is more(c) Because of control volume(d) Because it is moving with the flowThis question was addressed to me in homework.This key question is from Governing Equations in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» RIGHT option is (d) Because it is moving with the flow

To elaborate: As the control volume moves ALONG with the flow, their position COORDINATES continuously VARY with TIME. This needs a substantial derivative.
62.

Gauss divergence is applied to which of these terms?(a) Instantaneous total change of B inside the control mass(b) Instantaneous total change of B within the control volume(c) Net flow of B into and out of the control volume(d) Net flow of B into and out of the control massI had been asked this question in an interview.The query is from Governing Equations in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» RIGHT choice is (C) NET FLOW of B into and out of the control volume

The explanation: The term representing ‘net flow of B into and out of the control volume’ is a surface integral. This surface integral is converted into a volume integral using the Gauss divergence THEOREM.
63.

Let \(\hat{u}\) be the specific internal energy of a system moving along with the flow with a velocity \(\vec{V}\). What is the time rate of change of the total energy of the system per unit mass?(a) \(\hat{u}+\frac{1}{2}\vec{V}.\vec{V}\)(b) \(\frac{D}{Dt}(\hat{u}+\frac{1}{2}\vec{V}.\vec{V})\)(c) \(\frac{\partial}{\partial t}(\hat{u}+\frac{1}{2}\vec{V}.\vec{V})\)(d) \(\frac{D}{Dt}(\hat{u}+\vec{V}.\vec{V})\)The question was asked during an internship interview.My query is from Energy Equation topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» RIGHT answer is (B) \(\frac{D}{Dt}(\HAT{u}+\frac{1}{2}\vec{V}.\vec{V})\)

The best explanation: The total ENERGY of the system is

\(E=\hat{u}+\frac{1}{2}\vec{V}.\vec{V}\)

Take its substantial derivative as the model is not stationary.

rate of change of total energy=\(\frac{DE}{Dt}=\frac{D}{Dt}(\hat{u}+\frac{1}{2} \vec{V}.\vec{V})\).
64.

The energy equation should be solved to get this variable of the flow.(a) Velocity(b) Temperature(c) Density(d) PressureI had been asked this question in an internship interview.I'm obligated to ask this question of Energy Equation in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The CORRECT choice is (b) Temperature

The best I can explain: It is a MUST to solve the energy EQUATION when we WANT the temperature distribution of the system. The energy equation can give information about temperature.

65.

Consider an infinitesimally small fluid element with density ρ (of dimensions dx, dy and dz) fixed in space and fluid is moving across this element with a velocity \(\vec{V} = u\vec{i} + v\vec{j} + w\vec{k}\). The rate of change in mass of the fluid element is given by ____________(a) \(\frac{\partial(\rho u)}{\partial x} + \frac{\partial(\rho v)}{\partial y} + \frac{\partial(\rho w)}{\partial z}\)(b) \(\frac{\partial \rho}{\partial t}\)(c) \(\frac{\partial\rho}{\partial t}(dx \,dy \,dz) \)(d) \([\frac{\partial(\rho u)}{\partial x} + \frac{\partial(\rho v)}{\partial y} + \frac{\partial(\rho w)}{\partial z}]dx \,dy \,dz\)I got this question in homework.My enquiry is from Continuity Equation topic in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Right option is (c) \(\frac{\partial\rho}{\partial t}(DX \,DY \,dz) \)

To explain: Mass=density × volume

mass of fluid element=ρ×dx dy dz

rate of CHANGE in mass of fluid element=\(\frac{\partial\rho}{\partial t}dx \,dy \,dz \)

66.

Consider a model of finite control volume (volume V and surface area) fixed in space with elemental volume dV, vector elemental surface area d\(\vec{S}\), density ρ and flow velocity \(\vec{V}\). What is the mass inside the control volume?(a) \(\iint_s\rho \vec{V}.d\vec{S}\)(b) \(\iiint_V\rho dV\)(c) ρdV(d) \(\frac{\partial}{\partial t} \iiint_V\rho dV\)The question was asked in an interview.The doubt is from Continuity Equation in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct ANSWER is (B) \(\iiint_V\rho DV\)

To elaborate: Mass=density × volume

mass INSIDE dV=ρdV

mass inside \( V=\iiint_V\rho dV\).

67.

Substantial derivative = _____ + _____(a) Partial derivative, convective derivative(b) Local derivative, convective derivative(c) Local derivative, partial derivative(d) Total derivative, convective derivativeThis question was addressed to me in homework.I want to ask this question from Governing Equations topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Right option is (B) LOCAL DERIVATIVE, convective derivative

Explanation: SUBSTANTIAL derivative is the ADDITION of local derivative (based on fixed model) and convective derivative (based on motion of the model).

68.

Let \((\vec{V} \Delta t).\vec{ds}\) be the change in volume of elemental control volume in time Δt. Over the same time Δt, what is the change in volume of the whole control volume V with control surface S?(a) \(\int(\vec{V}\Delta t).\vec{ds}\)(b) \(\vec{V}\Delta t\)(c) \(\sum(\vec{V}\Delta t).\vec{ds}\)(d) \(\iint_s(\vec{V}\Delta t).\vec{ds}\)I had been asked this question in exam.My doubt is from Governing Equations in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The CORRECT answer is (d) \(\iint_s(\VEC{V}\Delta t).\vec{ds}\)

To elaborate: The CHANGE in volume of the WHOLE control volume is the summation of \((\vec{V} \Delta t).\vec{ds}\) over the total control surface S. This summation becomes integral as \(\vec{ds}\) is elemental. Therefore, \(\iint_s(\vec{V}\Delta t).\vec{ds}\) is the total change.

69.

In mathematical terms, how can the divergence of a velocity vector \((\vec{V})\) be represented?(a) \(\nabla.\vec{V}\)(b) \(\nabla\vec{V}\)(c) \(\nabla \times\vec{V}\)(d) \(\vec{V} \times\nabla\)The question was posed to me by my college professor while I was bunking the class.The doubt is from Governing Equations in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» CORRECT OPTION is (a) \(\nabla.\vec{V}\)

EASIEST explanation: \(\nabla.\vec{V}\)represents the divergence of a VECTOR. \(\nabla\vec{V}\) is gradient which is not possible for a vector. \(\nabla \times\vec{V}\) is the curl of a vector. \(\vec{V} \times\nabla\) does not represent any property.
70.

A finite control volume moving along with the flow __________(a) Has its position coordinates stationary(b) Has its particles moving into and out of it(c) Has the properties differentiated(d) Has the same particles always inside itThis question was addressed to me in a national level competition.Question is taken from Governing Equations topic in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct option is (d) Has the same particles ALWAYS inside it

To elaborate: As the finite control volume moves ALONG with the flow, the same particles are always CONCERNED. The mass inside this model also does not CHANGE.

71.

An equation modelled using infinitesimally small element leads to ____________(a) Partial differential equation(b) Integral equation(c) Differential equation(d) Linear differential equationI have been asked this question during an online interview.I need to ask this question from Governing Equations topic in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct choice is (a) Partial differential equation

The best explanation: Infinitesimally small element MODELS directly LEADS to a partial differential equation. The element is infinitesimal in the sense of differential calculus.

72.

Leibniz rule is applied to which of these terms in deriving Reynolds transport theorem?(a) Volume integral term of control volume(b) Differential term of material volume(c) Surface integral term of control volume(d) Volume integral term of material volumeI had been asked this question in an online interview.This intriguing question comes from Governing Equations topic in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct answer is (a) Volume integral term of control volume

To EXPLAIN: Using Leibniz rule, the DIFFERENTIATION of an integral term can be REDUCED. Here, differential of integral exists in the Volume integral term of Control Volume which is given by \(\frac{d}{dt}(\int_vb \rho dV).\)

73.

While converting the energy equation from one form to another, which of the following happens?(a) Either the left-hand side or the right-hand side of the equation changes(b) Both the left-hand side and the right-hand side of the equation change(c) The right-hand side of the equation changes(d) The left-hand side of the equation changesI have been asked this question in semester exam.I'd like to ask this question from Energy Equation topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct OPTION is (b) Both the LEFT-hand side and the right-hand side of the equation change

For explanation: Changes are applied to only left-hand side TERMS in the equations, but they affect both the left and right-hand sides of the equation.

74.

In Euler form of energy equations, which of these terms is not present?(a) Rate of change of energy(b) Heat radiation(c) Heat source(d) Thermal conductivityI had been asked this question in semester exam.The question is from Euler Equation topic in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Right CHOICE is (d) Thermal conductivity

Easy EXPLANATION: As the FLOW considered by Euler equations is ADIABATIC, heat cannot ENTER or exit the system. So, the thermal conduction is omitted.

75.

The major difference between the Navier-Stokes equations and the Euler equations is the dissipative transport phenomena. The impact of this phenomena in a system is ____(a) They decrease entropy(b) They increase entropy(c) They increase internal energy(d) They decrease internal energyI have been asked this question in an interview for job.Question is from Navier Stokes Equation topic in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct answer is (B) They increase entropy

To explain: Dissipation is the process where ENERGY is transformed from one form into ANOTHER. This TRANSFORMATION increases the entropy of the system.

76.

To convert the non-conservative integral equation of mass conservation into the conservative integral form, which of these theorems is used?(a) Stokes theorem(b) Kelvin-Stokes theorem(c) Gauss-Siedel theorem(d) Gauss Divergence TheoremThe question was posed to me by my college professor while I was bunking the class.The query is from Continuity Equation topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Right answer is (d) GAUSS Divergence Theorem

The best I can EXPLAIN: The expansion of non-conservative integral EQUATION gives two volume integral terms. One of these terms representing the mass flow is converted into SURFACE integral using the Gauss Divergence theorem.

77.

Consider a model of finite control volume (volume V and surface area) moving along the flow with elemental volume dV, vector elemental surface area d\(\vec{S}\), density ρ and flow velocity \(\vec{V}\). What is the time rate of change of mass inside the control volume?(a) \(\iiint_V\rho dV\)(b) \(\frac{\partial}{\partial t} \iiint_V\rho dV\)(c) \(\frac{D}{Dt} \iiint_V\rho dV\)(d) ρdVI have been asked this question in quiz.My doubt is from Continuity Equation in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Right option is (c) \(\frac{D}{DT} \iiint_V\rho dV\)

EXPLANATION: Substantial DERIVATIVE is USED as the model is moving.

mass=density × volume

mass inside dV=ρdV

mass inside \( V=\iiint_V\rho dV\)

time RATE of change of mass inside \(\frac{D}{Dt} \iiint_V\rho dV\).

78.

In terms of heat transfer, what does div(ΓgradΦ) mean?(a) Heat radiation(b) Heat convection(c) Thermal flow(d) Heat conductionThis question was posed to me in an internship interview.Question is from General Transport Equation in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct option is (d) Heat conduction

For explanation I WOULD say: Diffusive heat TRANSFER is called heat conduction. This refers to the process of heat transfer WITHOUT any movement of the particles.

79.

The simplified form of substantial derivative can be given by __________(a) \(\frac{DT}{Dt}=\frac{\partial T}{\partial t}+\nabla T\)(b) \(\frac{DT}{Dt}=\frac{\partial T}{\partial t}+\nabla .T\)(c) \(\frac{DT}{Dt}=\frac{\partial T}{\partial t}+\vec{V}.\nabla T\)(d) \(\frac{DT}{Dt}=\frac{\partial T}{\partial t}+\nabla \times T\)This question was addressed to me by my school teacher while I was bunking the class.My enquiry is from Governing Equations topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»
80.

What does this symbol Γ in the term div(ΓgradΦ) of the general transport equation mean?(a) Diffusion flux(b) Convection coefficient(c) Diffusion coefficient(d) Rate of diffusionThis question was addressed to me in an internship interview.The origin of the question is General Transport Equation in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» CORRECT ANSWER is (c) DIFFUSION coefficient

Easiest explanation: Γ represents the diffusion coefficient. The diffusion coefficient is DEFINED by Fick’s law of diffusion.
81.

Which of these is an acceptable tag for Lagrangian parcels?(a) Parcel’s centre of mass at instantaneous time(b) Parcel’s centre of pressure at instantaneous time(c) Parcel’s centre of mass at initial time(d) Parcel’s centre of pressure at initial timeI have been asked this question in an internship interview.Enquiry is from Governing Equations topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct answer is (c) Parcel’s centre of MASS at INITIAL time

To elaborate: Parcel’s centre of pressure is not suitable as it depends not only on position but on MANY variables too. INSTANTANEOUS time continuously varies along with the path. So, it cannot be a TAG.

82.

A control volume based model gives ___________ equation.(a) Integral(b) Differential(c) Conservative(d) Non-conservativeThis question was posed to me in homework.My question is from Governing Equations topic in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» CORRECT OPTION is (a) Integral

The explanation is: Control volumes are big ENOUGH that the FLOW properties can be integrated along it. Thus, a control volume yields an integral EQUATION.
83.

Relationship between thermodynamic variables of a flow field can be obtained through ___________(a) Momentum conservation(b) Thermodynamic equilibrium(c) Energy equations(d) Zeroth law of thermodynamicsThe question was asked in exam.Question is from Equations of State in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct choice is (B) Thermodynamic EQUILIBRIUM

The explanation: Thermodynamic equilibrium is a state of a matter where there is no transfer of energy. This condition can be USED to relate the thermodynamic properties with one ANOTHER.

84.

What are the dependent variables in the Navier-Stokes equations?(a) τ,T,p,ρ(b) p,ρ,T(c) u,v,w,T,p,ρ(d) u,v,w,T,pI had been asked this question in an internship interview.Question is taken from Navier Stokes Equation in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct choice is (c) u,v,w,T,p,ρ

For EXPLANATION: There are SIX DEPENDENT variables in the Navier-Stokes equations. They are PRESSURE (p), temperature (T), density (ρ) and three COMPONENTS of the velocity vector (u,v,w).

85.

Viscous forces fall into which kind of the following forces acting on a body?(a) Pressure force(b) Tensile force(c) Body forces(d) Surface forcesThe question was asked in semester exam.I'm obligated to ask this question of Governing Equations topic in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» RIGHT choice is (c) Body forces

For explanation I would say: The two TYPES of forces acting on a fluid are body forces and surface forces. Body forces are the forces produced by the fluid ELEMENT itself. Surface forces are the one acting on the fluid elements. VISCOUS forces act on the element and it comes under surface forces.
86.

Consider an infinitesimally small fluid element with density ρ (of dimensions dx, dy and dz with mass δ m and volume δ V) moving along with the flow with a velocity \(\vec{V}=u\vec{i}+v\vec{j}+w\vec{k}\). What is the time rate of change of mass of this element?(a) \(\frac{D(\rho \delta V)}{Dt}\)(b) \(\frac{\partial(\rho \delta m)}{\partial t}\)(c) \(\frac{\partial(\rho \delta V)}{\partial t}\)(d) \(\frac{D(\rho \delta m)}{Dt}\)I got this question in examination.This is a very interesting question from Continuity Equation in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» RIGHT answer is (a) \(\frac{D(\RHO \delta V)}{Dt}\)

EASIEST explanation: Substantial derivative is used as the model is moving.

mass = ρ δ V

time rate of CHANGE of mass=\(\frac{D(\rho \delta V)}{Dt}\)
87.

Equations of state provide the linkage between ___________ and ____________(a) Conservative, non-conservative equation(b) Eulerian, Lagrangian equations(c) Energy equation, mass and momentum equations(d) Differential, Integral equationsI got this question by my school teacher while I was bunking the class.The origin of the question is Equations of State in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Right CHOICE is (c) Energy equation, mass and momentum EQUATIONS

For EXPLANATION I would say: Equations of the state provide the linkage of Energy equation with mass and momentum equations. They give the thermodynamic properties in terms of the state VARIABLES.

88.

Among the unknowns of a flow field, some of the properties are given below. Which set contains only thermodynamic properties?(a) Density, pressure, specific internal energy, temperature(b) Density, velocity, specific internal energy, temperature(c) Velocity, pressure, specific internal energy, temperature(d) Density, pressure, specific internal energy, VelocityI have been asked this question in an international level competition.I want to ask this question from Equations of State topic in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct choice is (a) DENSITY, PRESSURE, specific internal energy, temperature

Explanation: Velocity is a PROPERTY completely RELATED to FLUID flow. The other properties – density, pressure, specific internal energy and temperature are thermodynamic.

89.

Which of these statements best defines local derivative?(a) Time rate of change(b) Spatial rate of change(c) Time rate of change of a moving point(d) Time rate of change at a fixed pointThis question was posed to me in an interview for job.My enquiry is from Governing Equations in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The CORRECT choice is (d) TIME rate of change at a fixed POINT

Best explanation: Local derivative is the term \(\frac{\PARTIAL}{\partial t}\) of a PROPERTY. This defines the time rate of change of a property at a particular point with the assumption that the point is fixed.

90.

In Lagrangian approach, the flow parcels follow __________(a) pressure field(b) velocity field(c) temperature field(d) density fieldThe question was posed to me during an interview for a job.Enquiry is from Governing Equations topic in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct option is (b) velocity field

To explain: Velocity field defines the MOTION of fluid. Parcels ALSO follow the same path of the fluid and THEREFORE, parcels can be SAID to follow the velocity field.

91.

The energy equation which is in terms of temperature can be changed to terms of internal energy using ___________(a) momentum equation(b) stress-strain relations(c) equations of state(d) continuity equationThis question was posed to me in a job interview.This interesting question is from Energy Equation in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct answer is (c) equations of state

The BEST explanation: Equations of state give the RELATIONSHIP between temperature and internal ENERGY which is i=Cv T. Using this RELATION, one can obtain the energy equation in internal energy TERMS.

92.

The Navier-Stokes equations are ____ system of equations.(a) coupled(b) uncoupled(c) exponential(d) radicalThis question was addressed to me by my school principal while I was bunking the class.My question comes from Navier Stokes Equation topic in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» RIGHT ANSWER is (a) coupled

For explanation I would say: Navier-Stokes equations are CALLED a coupled system of equations because all of the equations should be solved to get the dependent variables.Equations cannot be solved SEPARATELY to get the unknowns.
93.

Which among these forces used in momentum equation is a tensor?(a) Gravitational forces(b) Pressure forces(c) Viscous forces(d) Electromagnetic forcesI got this question by my school principal while I was bunking the class.I need to ask this question from Governing Equations topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The CORRECT CHOICE is (c) VISCOUS FORCES

The best I can explain: Viscous forces are tensors. The other forces given here (Gravitational, viscous and ELECTROMAGNETIC forces) are vectors.

94.

I am using an infinitesimally small element of fluid moving along with the flow as my model. What is the acceleration of this model in x-direction?(a) \(a_x=\frac{D\vec{V}}{Dt}\)(b) \(a_x=\frac{\partial \vec{V}}{\partial t}\)(c) \(a_x=\frac{Du}{Dt}\)(d) \(a_x=\frac{\partial u}{\partial t}\)This question was addressed to me at a job interview.The question is from Momentum Equation in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Right option is (c) \(a_x=\frac{DU}{DT}\)

Easy explanation: ACCELERATION is the rate of change of velocity. Acceleration in the x-direction is the rate of change of velocity in x-direction (u). As the MODEL is moving, rate of change is given by substantial derivative. Thus the acceleration in x-direction is \(a_x=\frac{Du}{Dt}\).

95.

Consider a small control volume V with the surface dS with a normal vector \(\vec{n}\). This moves in a fluid flow in time Δt into another position at a velocity \(\vec{V}\) (V in the diagram). What is the change in volume of this small control volume ΔV?(a) \([(\vec{V}\Delta t).\vec{n}]\)(b) \([(\vec{V}\Delta t).\vec{n}]dS\)(c) \([(\vec{V}\Delta t)]dS\)(d) \([(\vec{V}).\vec{n}]dS\)I had been asked this question in a job interview.The query is from Governing Equations in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct OPTION is (b) \([(\vec{V}\Delta t).\vec{n}]dS\)

The explanation is: The CHANGE in CONTROL VOLUME can be calculated as the volume of a cylinder with altitude \((\vec{V}\Delta t).\vec{n}\) (product of velocity and time) and BASE area dS.

96.

Divergence of velocity appears in the governing equations for _____________(a) infinitesimally small elements(b) stationary models(c) moving models(d) finite control volumesI have been asked this question by my college professor while I was bunking the class.Enquiry is from Governing Equations in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct option is (c) MOVING models

The best explanation: Divergence of velocity involves the CHANGE of VOLUME of the FLUID MODEL. For stationary models, volume does not change. So, this applies for only moving fluid elements.

97.

Other than finite control volume and infinitesimal small element, what is the third possible modelling of fluid flow?(a) Discrete approach(b) Quantum approach(c) Microscopic approach(d) Macroscopic approachesI had been asked this question during an interview.I'm obligated to ask this question of Governing Equations in chapter Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» CORRECT choice is (c) Microscopic approach

The best I can EXPLAIN: A microscopic approach is possible where the laws of nature are applied to the ATOMS and molecules. This is REGARDING KINETIC theory.
98.

What is the need of constructing a model for analysing fluids?(a) Fluids are not stationary but they have the same velocity in different parts(b) Fluids are stationary and they have the same velocity in different parts(c) Fluids are not stationary and they have different velocities in different parts(d) Fluids are not stationary but they have the same velocity in different partsI have been asked this question in my homework.I want to ask this question from Governing Equations in division Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

The correct choice is (C) Fluids are not stationary and they have DIFFERENT VELOCITIES in different parts

Easiest explanation: A solid body can be easily divided into different parts. A fluid is squishy and it has different velocities in different parts. This creates the need for a MODEL to analyse it.

99.

Which is/are the conservation laws that are enough to solve a complete fluid problem?(a) Energy and momentum conservation(b) Mass and energy conservation(c) Mass and momentum conservation(d) Mass equationThis question was addressed to me in an interview for job.This question is from Equations of State in section Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer» CORRECT OPTION is (c) MASS and momentum conservation

The best explanation: A complete fluid flow problem can OFTEN be solved by only using the mass and momentum conservation equations. Energy conservation equation is not necessary.
100.

The energy equation which is in terms of total energy can be changed to terms of internal energy using ___________(a) momentum equation(b) stress-strain relations(c) equations of state(d) continuity equationThis question was addressed to me during an interview.The doubt is from Energy Equation topic in portion Governing Equations of Fluid Dynamics of Computational Fluid Dynamics

Answer»

Correct choice is (a) momentum equation

To explain I would say: TOTAL energy is the sum of internal energy and kinetic energy. By some manipulation in the momentum equation, we can get the kinetic energy TERMS. If this is SUBTRACTED from the energy equation WRITTEN in total energy terms, we can get the same in terms of internal energy.